Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles
- Авторы: Krioukov V.1, Abdullin A.1, Nikandrova M.1, Safiullin I.1
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Учреждения:
- Tupolev Kazan National Research Technical University
- Выпуск: Том 61, № 4 (2018)
- Страницы: 682-686
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230782
- DOI: https://doi.org/10.3103/S1068799818040281
- ID: 230782
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Аннотация
The procedure of the reaction mechanism reduction including the DRGEP and engagement methods is considered and applied to the problem of calculating the non-equilibrium flows of propellant combustion products (kerosene + oxygen) in nozzles.
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Об авторах
V. Krioukov
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
A. Abdullin
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
M. Nikandrova
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
I. Safiullin
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: kazan711@yandex.ru
Россия, ul. Karla Marksa 10, Kazan, 420111